Sentence examples for lamina strength from inspiring English sources

Three design random variables with uncertainties were selected: (1) composite elastic constants; (2) lamina strength; and (3) the thickness of the helical and hoop layer.

It is based on micromechanical failure mechanisms but is expressed in terms of easily measured macroscopic lamina stiffness and strength properties.

The protein is part of the major protein network embedded in the basal lamina giving it strength interacting with integrin and the hemidesmo-somes and thereby supporting the strong interaction with the basal cells of the epidermis which is primarily through laminin of the basal lamina and integrin α4β6.

The Tsai Hill criterion is incorporated into the model for predicting failure strength of lamina and typical laminate in uniaxial tension and biaxial loading, respectively.

The present study also shows that the nonlinear hardening behavior of matrix reflects more realistically the influence of plastic deformations on the in situ transverse strength of lamina than the perfectly plastic behavior of matrix.

Uncertainties arising in the mechanical properties and ultimate strengths of one lamina are modeled as random variables and considered in the process of probabilistic strength prediction.

The elastic modulus and ultimate strength of each lamina were predicted based on micromechanics.

Simplified micromechanics equations are used to estimate the stiffnesses and strength of each lamina using the fiber volume fraction and material properties of the matrix and fibers.

It was evident from the finite element analysis and cadaveric testing that the introduction of the hinge reduced the strength of the lamina by 5- to 9-fold depending on the direction of loading.

Although the impact damage resistance of GLARE is better than its individual constituents i.e. aluminum and glass/epoxy composites, the poor strength of the lamina's interfaces causes failure modes such as delamination and debonding.

The theoretical results demonstrate that the final failure mode of an angle-ply laminate is determined by the value of a failure factor which is related to the thickness and strength of the lamina, the width and ply angle of the laminate, and the interface strength.